Unformatted text preview: V ? Explain your method to determine this from the results of part 1. 3. Approximately how far beyond the wingtip is the upwash in excess of 1% of V ? Explain your method to determine this from the results of part 1. Note: the real 737800 has a swept and tapered wing which requires more detailed modeling than a single horseshoe vortex. Also, the cruise Mach number of 0.785 is in the compressible subsonic regime which we will address the last week or two of the semester. Nevertheless, I wanted some “real numbers” for you to observe in the results. The results will be approximate and in the right order of magnitude....
View
Full
Document
This note was uploaded on 02/21/2012 for the course AAE 334 taught by Professor Collicott during the Fall '09 term at Purdue.
 Fall '09
 COLLICOTT

Click to edit the document details